DELTA 2 R/B

Satellite information

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Satellite Type and Status

ROCKET BODYIN ORBIT

Key statistics

Satellite DELTA 2 R/B at a glance.

Uptime

10345

Days in orbit

Revolutions

≈ 14.5

Per day

Orbit

LEO

Low Earth Orbit

Inclination

86.9

Latest

Satellite identification and parameters

Extended collection of information and parameters for DELTA 2 R/B.

Object identification

Identified? True

Debris? False

Object name: DELTA 2 R/B

International designator: 1997-020F

Object number (NORAD): 24797

Object ID (CCSDS): 24797

Country: UNITED STATES OF AMERICA (US)

Current information (Y/N): Y

RCS size: LARGE

Orbital parameters

Period: 99.487 minutes

Inclination: 86.8996 deg

SMA: 7112.196 km

Apoapsis: 888.371 km

Periapsis: 579.751 km

RAAN: 334.5562 deg

Eccentricy: 0.02169659

Argument of periapsis: 34.337 deg

Mean anomaly: 77.8176 deg

Mean motion: 14.47428744 rev/day

Mean motion (dot): 0.00000841 rev/day2

B* drag term: 0.00016502404 1/REarth

Two-line elements (TLE)

Creation date: Aug. 31, 2025, 2:26 a.m.

Reference frame: TEME

Reference center: EARTH

Epoch: Aug. 30, 2025, 6:41 p.m. UTC

TLE line 0: 0 DELTA 2 R/B

TLE line 1: 1 24797U 97020F 25242.77865041 .00000841 00000-0 16502-3 0 9990

TLE line 2: 2 24797 86.8996 334.5562 0216966 34.3370 77.8176 14.47428744490571

Live tracking on map

Real-time ground track for satellite DELTA 2 R/B.

In-orbit conjunctions

A list of the most updated potential collisions computed for object DELTA 2 R/B.

Target Orbit TCA Probability of collision Miss distance Type
FENGYUN 1C DEB SSO 2025-08-28 14:22:11 0.0002447958 613.0 (m) DEBRIS
ATLAS CENTAUR R/B LEO 2025-08-06 04:13:01 0.0002892782 339.0 (m) ROCKET BODY
CZ-6A DEB LEO 2025-04-12 12:39:54 0.0001936757 341.0 (m) DEBRIS
COSMOS 1867 COOLANT LEO 2024-12-10 05:31:29 0.0001435911 832.0 (m) DEBRIS
NOAA 16 DEB SSO 2024-11-14 02:49:57 0.000231766 408.0 (m) DEBRIS

Associated space launch

Iridium provides global mobile telecommunications services using a constellation of 66 low earth orbit satellites in a 86.4° inclined orbit. Although 77 satellites were originally envisioned for the system and spawned the name based on the 77th element in the periodic table, the system has been scaled back. Motorola's Satellite Communications Group designed and manufactured the Iridium satellites with Lockheed Martin providing the LM-700A spacecraft buses.

DELTA 2 R/B was lifted into orbit during the mission ‘Delta II | Iridium 04 to 08’, on board a Delta II space rocket.

The launch took place on May 5, 1997, 2:55 p.m. from Space Launch Complex 2W.

For more information about the launch, click the button.

Launch to space Delta II | Iridium 04 to 08
Delta II | Iridium 04 to 08

Agency: N/A

Status: Launch Successful

Launch date: May 5, 1997, 2:55 p.m. UTC

Rocket: Delta II

Launch pad: Space Launch Complex 2W

Location: Vandenberg SFB, CA, USA

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